The system (17) has an electrical network (20) to electrically power functional equipment (14A-14F) of an aircraft (10). A regulating assembly (24) includes a secondary electrical power source (58) formed by a fuel cell (70), and a conversion assembly (60) for additional electrical power injected on the electrical network. The conversion assembly consumes the additional electrical power to create a supply fluid for the fuel cell. Reservoirs (62A, 62B) are inserted between the conversion assembly and the fuel cell to collect the supply fluid produced by the conversion assembly. An independent claim is also included for an electricity management method for an aircraft.


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    Title :

    Système électrique d'aéronef et procédé de gestion associé


    Additional title:

    Aircraft electrical system and related management method
    Elektrisches System eines Luftfahrzeugs und entsprechendes Steuerungsverfahren


    Contributors:

    Publication date :

    2016-06-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / B60R Fahrzeuge, Fahrzeugausstattung oder Fahrzeugteile, soweit nicht anderweitig vorgesehen , VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05F SYSTEMS FOR REGULATING ELECTRIC OR MAGNETIC VARIABLES , Systeme zum Regeln elektrischer oder magnetischer Veränderlicher



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